As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A SCHEDULE INSPECTION, PERFORMED INSPECTION IAW SB 57-88, WINGS - PLATES/SKIN - INSPECT/REPAIR/MODIFY LOWER INBOARD AFT WING SKIN PANEL. FOUND HOLES 1 AND A BOTTOM AFT LEFT WING SKIN AT STA 69.5 WERE FOUND CRACKED AS INDICATED BY NDT INSPECTION. REPAIRED IAW SB 57-88 AND TIMCO ENGINEERING SKETCH REO-04502.